Patents by Inventor Victor J. Barackman

Victor J. Barackman has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 10247318
    Abstract: Fluid apparatus and related methods are disclosed. An example fluid apparatus includes a housing defining a fluid flow passageway between an inlet and an outlet. The housing has a first valve seat and a second valve seat positioned in the fluid flow passageway. The first valve seat is spaced from the second valve seat. A flow control member is positioned in the fluid flow passageway. The flow control member has a first disk and a second disk. The first disk is to engage the first valve seat and the second disk to engage the second valve seat.
    Type: Grant
    Filed: August 4, 2016
    Date of Patent: April 2, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Christopher C. Veto, Gary D. Grayson, Victor J. Barackman
  • Patent number: 10184579
    Abstract: Fluid apparatus and related methods are disclosed. An example fluid apparatus includes a valve body defining a fluid flow passageway and a plurality of valve seats. A flow control member is positioned in the fluid flow passageway of the valve body. The flow control member having a plurality of disks. A respective one of the disks moves relative to a respective one of the valve seats to control fluid flow through the valve body. The flow control member is adjustable relative to a longitudinal axis of the valve body to provide a preload to the disks. Each of the disks has a cracking pressure corresponding to the preload.
    Type: Grant
    Filed: August 4, 2016
    Date of Patent: January 22, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Christopher C. Veto, Gary D. Grayson, Victor J. Barackman
  • Patent number: 9993778
    Abstract: A diffuser is disclosed and includes a channel with an inner portion having an inlet and an outlet through which a gaseous substance enters and exits the diffuser, respectively. The inner portion includes a first conical section that has an increasing cross-sectional area, taken along a plane perpendicular to a central axis, in a first direction. The inner portion also includes a second conical section that has a decreasing cross-sectional area, taken along a plane perpendicular to the central axis, in the first direction. The second conical section is communicatively coupled with the first conical section. The outer portion includes a first annular section that has an increasing cross-sectional area, taken along a plane perpendicular to the central axis, in a second direction opposite the first direction. The diffuser further includes a plurality of orifices that communicatively couple the second conical section with the first annular section.
    Type: Grant
    Filed: June 8, 2016
    Date of Patent: June 12, 2018
    Assignee: The Boeing Company
    Inventors: Gary D. Grayson, Martin E. Lozano, Victor J. Barackman
  • Publication number: 20180038498
    Abstract: Fluid apparatus and related methods are disclosed. An example fluid apparatus includes a valve body defining a fluid flow passageway and a plurality of valve seats. A flow control member is positioned in the fluid flow passageway of the valve body. The flow control member having a plurality of disks. A respective one of the disks moves relative to a respective one of the valve seats to control fluid flow through the valve body. The flow control member is adjustable relative to a longitudinal axis of the valve body to provide a preload to the disks. Each of the disks has a cracking pressure corresponding to the preload.
    Type: Application
    Filed: August 4, 2016
    Publication date: February 8, 2018
    Inventors: Christopher C. Veto, Gary D. Grayson, Victor J. Barackman
  • Publication number: 20180038497
    Abstract: Fluid apparatus and related methods are disclosed. An example fluid apparatus includes a housing defining a fluid flow passageway between an inlet and an outlet. The housing has a first valve seat and a second valve seat positioned in the fluid flow passageway. The first valve seat is spaced from the second valve seat. A flow control member is positioned in the fluid flow passageway. The flow control member has a first disk and a second disk. The first disk is to engage the first valve seat and the second disk to engage the second valve seat.
    Type: Application
    Filed: August 4, 2016
    Publication date: February 8, 2018
    Inventors: Christopher C. Veto, Gary D. Grayson, Victor J. Barackman
  • Publication number: 20170354935
    Abstract: A diffuser is disclosed and includes a channel with an inner portion having an inlet and an outlet through which a gaseous substance enters and exits the diffuser, respectively. The inner portion includes a first conical section that has an increasing cross-sectional area, taken along a plane perpendicular to a central axis, in a first direction. The inner portion also includes a second conical section that has a decreasing cross-sectional area, taken along a plane perpendicular to the central axis, in the first direction. The second conical section is communicatively coupled with the first conical section. The outer portion includes a first annular section that has an increasing cross-sectional area, taken along a plane perpendicular to the central axis, in a second direction opposite the first direction. The diffuser further includes a plurality of orifices that communicatively couple the second conical section with the first annular section.
    Type: Application
    Filed: June 8, 2016
    Publication date: December 14, 2017
    Inventors: Gary D. Grayson, Martin E. Lozano, Victor J. Barackman
  • Patent number: 7946534
    Abstract: A spacecraft pressure vessel has a tub member. A sidewall member is coupled to the tub member so that a bottom section of the sidewall member extends from an attachment intersection with the tub member and away from the tub member. The bottom section of the sidewall member receives and transfers a load through the sidewall member.
    Type: Grant
    Filed: October 24, 2007
    Date of Patent: May 24, 2011
    Assignee: The Boeing Company
    Inventors: Xavier D. Simon, Victor J. Barackman
  • Publication number: 20090108137
    Abstract: A spacecraft pressure vessel has a tub member. A sidewall member is coupled to the tub member so that a bottom section of the sidewall member extends from an attachment intersection with the tub member and away from the tub member. The bottom section of the sidewall member receives and transfers a load through the sidewall member.
    Type: Application
    Filed: October 24, 2007
    Publication date: April 30, 2009
    Inventors: Xavier D. Simon, Victor J. Barackman
  • Patent number: 7334844
    Abstract: A two-part seat (10) providing full body support that is specific for each crew member (30) on an individual basis. The two-part construction for the seat (10) can accommodate many sizes and shapes for crewmembers (30) because it is reconfigurable and therefore reusable for subsequent flights. The first component of the two-part seat construction is a composite shell (12) that surrounds the crewmember's entire body and is generically fitted to their general size in height and weight. The second component of the two-part seat (10) is a cushion (20) that conforms exactly to the specific crewmember's entire body and gives total body support in more complex environment.
    Type: Grant
    Filed: January 6, 2005
    Date of Patent: February 26, 2008
    Assignee: The Boeing Company
    Inventors: Victor J. Barackman, John K. Pulley, Xavier D. Simon, Sandra D. McKee